DocumentCode
1880965
Title
Innovative astronaut navigation system based on smart integrated sensors
Author
Benzerrouk, Hamza ; Nebylov, Alexander ; Yatsevitch, Gennady
Author_Institution
IIAAT, Algeria
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
9
Abstract
Original algorithms for navigation on the surface of Mars planet, especially applied to astronauts, are proposed in this paper. The autonomous navigation system for astronaut is based on inertial measurement unit (redundant) and Laser (redundant), which permits to localize and navigate in known environment and unknown environment constructing its map in real time, using adaptive algorithms and physical and natural constraints of astronaut´s body. The estimation of the position of astronauts is done using non linear adaptive filters such as the Extended Kalman Filter (EKF) and other non linear variant filters. Finally, additional smart idea is to use Phobos and Deimos as navigation constellation in addition to one more satellite.
Keywords
Kalman filters; Mars; adaptive filters; navigation; nonlinear filters; planetary satellites; sensors; EKF; Mars planet; adaptive algorithms; extended Kalman Filter; innovative astronaut navigation system; navigation constellation; non linear variant filters; satellite; smart integrated sensors; Earth; Estimation; Gravity; Laser radar; Mars; Satellite navigation systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187112
Filename
6187112
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